The invention discloses a double-duct vertical take-off and landing electric aircraft which comprises a frame body, duct power systems, a battery and a riding control system are arranged on the frame body, the duct power systems are arranged at the left end and the right end of the frame body, and the riding control system is arranged at the front end of the frame body. The battery is arranged at the rear end of the frame body and used for providing energy power for the duct power system and the driving and riding control system. The aircraft is simple in structure and convenient to use, the whole aircraft adopts a quick disassembly and assembly mode, the whole assembly process is simple and quick, a good safety protection effect can be provided for each part during transportation, collision and other situations are avoided, energy power is provided for the duct power system and the driving and riding control system through the battery, and the safety of the aircraft is improved. A driver and passengers can control the duct power system through the riding control system, the ducts at the two side ends generate thrust downwards at the same time, the aircraft can fly upwards, the flight direction can be changed through the flow guide assembly, and therefore steering of the aircraft is completed.
本发明公开了一种双涵道垂直起降电动飞行器,包括有架体,所述架体上设有涵道动力系统、电池和驾乘控制系统,所述涵道动力系统设于架体的左右两端,所述驾乘控制系统设于架体的前端,所述电池设于架体的后端并用于向涵道动力系统及驾乘控制系统提供能源动力;本发明结构简单、使用方便,整个飞行器采用快速拆装的方式,整个组装过程简单快捷,且运输时能够对每个部件都提供良好的安全保护效果,避免发生碰撞等情况,通过电池对涵道动力系统和驾乘控制系统提供能源动力,使得驾乘人员能够通过驾乘控制系统控制涵道动力系统,并使得两侧端的涵道同时向下方产生推力,使飞行器能够向上飞,并且还能通过导流组件改变飞行方向,从而完成飞行器的转向。
Double-duct vertical take-off and landing electric aircraft
一种双涵道垂直起降电动飞行器
2024-12-20
Patent
Electronic Resource
Chinese
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